# N930DN: 1996 Mcdonnell Douglas MD-90-30

- Status: Valid registration
- Airframe: [Mcdonnell Douglas MD-90-30](https://openairdocs.org/model/mcdonnell-douglas-md-90-30) (registry code 3023690, 142 seats)
- Engine: [IAE V2500SERIES](https://openairdocs.org/engine/iae-v2500series) (registry code 34601)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 53458
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: January 13, 2012
- Certificate issued: December 2, 2015
- Expires: December 31, 2028
- Mode S code: ACE601
- Registered owner: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=930DN
- Page: https://openairdocs.org/aircraft/N930DN

From the FAA registry file of October 22, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 91 in force

### Matched by airframe (Mcdonnell Douglas MD-90-30)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2019-24-17](https://openairdocs.org/ad/2019-24-17): Wings · Boeing MD-90-30. Effective Jan 24, 2020
- [AD 2018-07-04](https://openairdocs.org/ad/2018-07-04): Ice and rain protection · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 3 more. Effective Sep 10, 2018
- [AD 2018-03-04](https://openairdocs.org/ad/2018-03-04): Airspeed/Mach Indicator · Boeing 717-200, DC-9-11, DC-9-12 and 23 more. Effective Mar 16, 2018
- [AD 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 2017
- [AD 2017-11-02](https://openairdocs.org/ad/2017-11-02): Stabilizers · Boeing MD-90-30. Effective Jun 27, 2017
- [AD 2016-25-26](https://openairdocs.org/ad/2016-25-26): Navigation · Boeing MD-90-30. Effective Feb 2, 2017
- [AD 2016-22-18](https://openairdocs.org/ad/2016-22-18): Fuselage · Boeing MD-90-30. Effective Nov 21, 2016
- [AD 2016-03-06](https://openairdocs.org/ad/2016-03-06): Fuel · Boeing DC-9-11, DC-9-12, DC-9-13 and 21 more. Effective Mar 23, 2016
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-24-03](https://openairdocs.org/ad/2014-24-03): Stabilizers · Boeing MD-90-30. Effective Jan 27, 2015
- [AD 2014-24-04](https://openairdocs.org/ad/2014-24-04): Stabilizers · Boeing MD-90-30. Effective Jan 13, 2015
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2012-22-04](https://openairdocs.org/ad/2012-22-04): Wings · Boeing MD-90-30. Effective Dec 5, 2012
- [AD 2012-21-18](https://openairdocs.org/ad/2012-21-18): Wings · Boeing MD-90-30. Effective Dec 5, 2012
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-12-12](https://openairdocs.org/ad/2011-12-12): Stabilizers · Boeing MD-90-30. Effective Jul 22, 2011
- [AD 2011-06-12](https://openairdocs.org/ad/2011-06-12): Stabilizers · Boeing MD-90-30. Effective Apr 26, 2011
- [AD 2011-03-09](https://openairdocs.org/ad/2011-03-09): Ignition · Boeing MD-90-30. Effective Mar 14, 2011
- [AD 2011-01-11](https://openairdocs.org/ad/2011-01-11): Stabilizers · Boeing MD-90-30. Effective Feb 9, 2011
- [AD 2010-25-04](https://openairdocs.org/ad/2010-25-04): Compliance · Boeing DC-9-31, DC-9-32, DC-9-32 (VC-9C) and 14 more. Effective Jan 11, 2011
- [AD 2010-22-04](https://openairdocs.org/ad/2010-22-04): Nacelles/Pylons · Boeing MD-90-30. Effective Dec 3, 2010
- [AD 2010-21-16](https://openairdocs.org/ad/2010-21-16): Hydraulic Power · Boeing MD-90-30. Effective Nov 18, 2010
- [AD 2010-16-11](https://openairdocs.org/ad/2010-16-11): Wings · Boeing MD-90-30. Effective Sep 22, 2010
- [AD 2009-15-16 R1](https://openairdocs.org/ad/2009-15-16-R1): Doors · Intrusion/Penetration Resistance Flightdeck Door and Reinforced… (Aircraft Reconfig Technologies STC ST02463AT). Effective Aug 5, 2010
- [AD 2010-05-04](https://openairdocs.org/ad/2010-05-04): Fuselage · Boeing MD-90-30. Effective Apr 1, 2010
- [AD 2009-21-10 R1](https://openairdocs.org/ad/2009-21-10-R1): Oxygen · Airbus A300 B4-605R, A300 B4-620, A300 B4-622 and 138 more. Effective Feb 4, 2010
- [AD 2009-13-08](https://openairdocs.org/ad/2009-13-08): Stabilizers · Boeing MD-90-30. Effective Aug 3, 2009
- [AD 2009-11-11](https://openairdocs.org/ad/2009-11-11): Fuel · Boeing MD-90-30. Effective Jul 7, 2009
- [AD 2008-11-15](https://openairdocs.org/ad/2008-11-15): Fuel tank systems · Boeing 717-200, DC-9-11, DC-9-12 and 21 more. Effective Jul 3, 2008
- [AD 2008-06-27](https://openairdocs.org/ad/2008-06-27): Evacuation system's shear-pin · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 91 more. Effective Apr 28, 2008
- [AD 2007-17-19](https://openairdocs.org/ad/2007-17-19): Static port heater assemblies · Boeing MD-90-30. Effective Oct 2, 2007
- [AD 2006-16-09](https://openairdocs.org/ad/2006-16-09): Refueling manifold in the right wing refueling station area · Boeing MD-90-30. Effective Sep 13, 2006
- [AD 2006-10-14](https://openairdocs.org/ad/2006-10-14): Stop pad support fittings · Boeing 717-200, DC-9-11, DC-9-12 and 22 more. Effective Jun 21, 2006
- [AD 2006-07-11](https://openairdocs.org/ad/2006-07-11): Aft attach fitting assembly of the spoiler link · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 3 more. Effective May 5, 2006
- [AD 2006-01-02](https://openairdocs.org/ad/2006-01-02): Upper lock link assembly of the nose landing gear (NLG) · Boeing DC-9-14, DC-9-15, DC-9-15F and 18 more. Effective Feb 22, 2006
- [AD 2005-13-14](https://openairdocs.org/ad/2005-13-14): Dual anti-skid control manifolds (DACM) · Boeing MD-90-30. Effective Jul 29, 2005
- [AD 2005-09-08](https://openairdocs.org/ad/2005-09-08): Aft left lavatory · Boeing MD-90-30. Effective May 20, 2005
- [AD 2005-06-03](https://openairdocs.org/ad/2005-06-03): fluorescent light lamp holders · Boeing MD-90-30. Effective Apr 20, 2005
- [AD 2005-05-02](https://openairdocs.org/ad/2005-05-02): Electrical/electronics (E/E) compartment · Boeing MD-90-30. Effective Apr 6, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-07-12](https://openairdocs.org/ad/2004-07-12): Terminal studs on the 3-phase limiter blocks · Boeing MD-90-30. Effective May 11, 2004
- [AD 2004-05-25](https://openairdocs.org/ad/2004-05-25): Seat Locking Pins · Boeing DC-9-14, DC-9-15, DC-9-15F and 18 more. Effective Apr 19, 2004
- [AD 2004-05-18](https://openairdocs.org/ad/2004-05-18): Main Landing Gear (MLG) · Boeing MD-90-30. Effective Apr 13, 2004
- [AD 2004-05-03](https://openairdocs.org/ad/2004-05-03): Shock strut cylinders · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 3 more. Effective Mar 15, 2004
- [AD 2003-26-07](https://openairdocs.org/ad/2003-26-07): Circuit Breakers · Boeing MD-90-30. Effective Feb 4, 2004
- [AD 2003-11-15 R1](https://openairdocs.org/ad/2003-11-15-R1): Pressure relief door · Boeing MD-90-30. Effective Jan 27, 2004

### Matched by engine (IAE V2500SERIES)

None in force.

### Historical (superseded or no longer in force)

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2012-18-05](https://openairdocs.org/ad/2012-18-05) (historical): Fuel · Boeing DC-9-11, DC-9-12, DC-9-13 and 21 more. Effective Oct 11, 2012
- [AD 2009-15-16](https://openairdocs.org/ad/2009-15-16) (historical): Doors · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 18 more. Effective Jul 6, 2010
- [AD 2009-21-10](https://openairdocs.org/ad/2009-21-10) (historical): Oxygen · Airbus A300, Model B4-605R, A300, Model B4-620, A300, Model B4-622 and 138 more. Effective Dec 17, 2009
- [AD 2009-07-04](https://openairdocs.org/ad/2009-07-04) (historical): Auxiliary hydraulic power system · McDonnell Douglas MD-90-30. Effective May 5, 2009
- [AD 2008-18-10](https://openairdocs.org/ad/2008-18-10) (historical): Aft mount support fitting · McDonnell Douglas MD-90-30. Effective Sep 24, 2008
- [AD 2005-03-05](https://openairdocs.org/ad/2005-03-05) (historical): Aft left lavatory · Boeing MD-90-30. Effective Feb 22, 2005
- [AD 2003-17-07](https://openairdocs.org/ad/2003-17-07) (historical): Fire Extinguishers for the Engine and Auxiliary Power Unit (APU) · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 60 more. Effective Sep 24, 2003
- [AD 2003-11-15](https://openairdocs.org/ad/2003-11-15) (historical): Pressure relief door for the thrust reverser · McDonnell Douglas MD-90-30. Effective Jul 9, 2003
- [AD 2003-04-10](https://openairdocs.org/ad/2003-04-10) (historical): Wire Chafing · McDonnell Douglas MD-90-30. Effective Apr 4, 2003
- [AD 2003-03-15](https://openairdocs.org/ad/2003-03-15) (historical): Airplane Flight Manual (AFM) - Oxygen Masks · Boeing 707 Series (all), 720 Series (all), 727 Series (all) and 75 more. Effective Mar 7, 2003
- [AD 2001-07-10](https://openairdocs.org/ad/2001-07-10) (historical): Airplane Flight Manual - Landing Field Length · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 3 more. Effective Apr 27, 2001
- [AD 2000-20-04](https://openairdocs.org/ad/2000-20-04) (historical): Electrical Power Control Unit (EPCU) · McDonnell Douglas MD-90-30. Effective Nov 13, 2000
- [AD 2000-16-01](https://openairdocs.org/ad/2000-16-01) (historical): Electrical Power Control Unit (EPCU) · McDonnell Douglas MD-90-30. Effective Sep 19, 2000
- [AD 2000-15-17](https://openairdocs.org/ad/2000-15-17) (historical): Hydraulic Pipe Assembly in the Aft Fuselage · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 3 more. Effective Sep 12, 2000
- [AD 2000-03-08](https://openairdocs.org/ad/2000-03-08) (historical): Main Landing Gear (MLG) Piston · McDonnell Douglas MD-90-30. Effective Mar 22, 2000
- [AD 2000-03-51](https://openairdocs.org/ad/2000-03-51) (historical): Jackscrew Assembly · McDonnell Douglas 717-200, DC-9 Series (all), MD-88 and 1 more. Effective Mar 6, 2000
- [AD 99-13-07](https://openairdocs.org/ad/99-13-07) (historical): Main Landing Gear Shock Strut Pistons · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 3 more. Effective Jul 28, 1999
- [AD 97-11-07](https://openairdocs.org/ad/97-11-07) (historical): Structural Integrity · Boeing MD-90-30. Effective Jun 26, 1997
- [AD 95-04-01](https://openairdocs.org/ad/95-04-01) (historical): AFM - Limitations - Windshear · Boeing 727-100 Series, 727-200 Series, 737-100 Series and 54 more. Effective Mar 8, 1995

All 112: https://openairdocs.org/aircraft/N930DN/ads.md

## Information bulletins (advisory) (4 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-18-33](https://openairdocs.org/saib/NM-18-33): Engine Fuel and Control. Issued Dec 17, 2018
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006

## NTSB investigations

None matched to N930DN.

## FAA accident and incident reports

None matched to N930DN.

## Service difficulty reports (122, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DALA2019073004488](https://openairdocs.org/sdr/DALA2019073004488), Jul 29, 2019: LINK. WORN. LOUD NOISE FROM NOSE GEAR DOOR AREA BEGAN ON CLIMBOUT ABOUT 15,000 FT. MTC. ADVISED CYCLING GEAR AT 25,000 FT. RED GEAR DOOR LIGHT ILLUM. WITH GEAR UP, RETURNED
- [SDR DALA2019051603028](https://openairdocs.org/sdr/DALA2019051603028), May 15, 2019: PSEU. MALFUNCTIONED. LANDING GREEN LIGHTS DID NOT ILLUM. WHEN GEAR HANDLE DOWN. RAN CHECK LIST AND GOT 3 GREEN WITH EMERG. EXT HANDLE. STOPPED ON RNWY. MTC MEET A/C ON RNWY. PINNED 
- [SDR DALA20190402083](https://openairdocs.org/sdr/DALA20190402083), Mar 30, 2019: BATTERY. INOPERATIVE. OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY RECHARGEABLE POWER SUPPLY AND BATTERY PER MD90 WDM 33-51-13 AND MD90 AMM 33-51-03. (LP# 1008754)
- [SDR DALA2019012400490](https://openairdocs.org/sdr/DALA2019012400490), Jan 23, 2019: POWER SUPPLY. INOPERATIVE. EXTERIOR O'WING EMERGENCY LIGHTS INOP. REPLACED OVERWING EMERGENCY LIGHTS POWER SUPPLY AND BATTERY. AMM 33-51. CKS GOOD. OK FOR SERVICE. (LP# 0915674)
- [SDR DALA2018062604225](https://openairdocs.org/sdr/DALA2018062604225), Jun 24, 2018: PANEL. MISSING. PANEL MISSING ON THE NR 1 ENGINE PYLON. INSTALLED A REPLACEMENT PANEL IAW AMM 20-10. OK FOR SERVICE.
- [SDR DALA2017061904856](https://openairdocs.org/sdr/DALA2017061904856), Jun 16, 2017: LANYARD. DETACHED. GIRT BAR LANYARD DETACHED FROM EMERGENCY SLIDE PACK L1 DOOR. SECURED LANYARD. OPERATION CHECKS GOOD.
- [SDR DALA2017040502835](https://openairdocs.org/sdr/DALA2017040502835), Apr 3, 2017: DOOR FRAME. DENTED. SMALL DENT IN L1 DOOR FRAME. STRAIGHTENED LOWER EDGE IAW SRM 52-01-01.
- [SDR DALA2017012600695](https://openairdocs.org/sdr/DALA2017012600695), Jan 21, 2017: WIRE. ARCED. DIVERTED DUE TO A STRAKE ICE FAULT ON EOAP DURING FLIGHT, WITH ICING CONDITIONS FORECASTED. MAINTENANCE REMOVED AND REPLACED THE RIGHT STRAKE WITH NO HELP. MAIN
- [SDR DALA2016122210119](https://openairdocs.org/sdr/DALA2016122210119), Dec 21, 2016: SLIDE. MALFUNCTIONED. TAIL CONE SLIDE UNFOLDED WHEN REMOVED FOR TAIL CONE FUNCTION. INSTALLED TAIL CONE SLIDE.
- [SDR DALA2016123010189](https://openairdocs.org/sdr/DALA2016123010189), Dec 20, 2016: BATTERY PACK. DISCHARGED. EMERGENCY EXIT SIGNS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT STA 740. OPERATIONAL TEST CHECK GOOD.
- [SDR DALA2016111808977](https://openairdocs.org/sdr/DALA2016111808977), Nov 16, 2016: FRAME. CRACKED. CANTED FRAME, STA 1520, WEB CRACKED AT UPPER LEFT CORNER OF CUT OUT. REPAIRED IAW ERA 52770-14.
- [SDR DALA2016110908368](https://openairdocs.org/sdr/DALA2016110908368), Nov 2, 2016: GLOWSTRIP. MISSING. PHOTO LUMINESCENT STRIP MISSING AT 27B. REPLACED STRIP IAW MM. PLACARD REMOVED.
- [SDR DALA2016101007214](https://openairdocs.org/sdr/DALA2016101007214), Oct 5, 2016: ACTUATOR. FAILED. UN-COMMANDED MOVEMENT OF SPOILER HANDLE ON TAKE-OFF. PERFORMED OPERATIONAL TEST OF THE GROUND SPOILER AUTOMATIC ACTUATOR PER MM. REMOVED AND REPLACED GROUND SPO
- [SDR DALA2016062304984](https://openairdocs.org/sdr/DALA2016062304984), Jun 23, 2016: HINGE FITTING. DAMAGED. HORIZONTAL STABILIZER AT LT VERTICAL STABILIZER HINGE ATTACH FITTINGS, PITTED WITH MATERIAL LOSS ON OUTER AND INNER SURFACE. ALSO ON INNER BUSHING BORES.
- [SDR DALA2016062304983](https://openairdocs.org/sdr/DALA2016062304983), Jun 23, 2016: HINGE FITTING. DAMAGED. HORIZONTAL STABILIZER RT HINGE FITTINGS PITTED WITH MATERIAL LOSS ON OUTER AND INNER SURFACE. CORROSION CONTAINED. FABRICATED AND INSTALLED IAW SRM 55-30-05.
- [SDR DALA2016062804976](https://openairdocs.org/sdr/DALA2016062804976), Jun 23, 2016: SPAR. CRACKED. NR 4 HORIZONTAL STABILIZER LT SIDE AFT REAR SPAR UPPER AFT BARREL NUT HOLE CORRODED, CRACK INDICATION. REMOVED HORIZONTAL STABILIZER UNSERVICEABLE.
- [SDR DALA2016050903899](https://openairdocs.org/sdr/DALA2016050903899), May 5, 2016: DOOR FRAME. DAMAGED. NLG OPENING AFT RT SIDE FRAME DAMAGED. INSTALLED NEW FRAME IAW DWG 5913421.
- [SDR DALA2016050903898](https://openairdocs.org/sdr/DALA2016050903898), May 5, 2016: BUSHING. CORRODED. LEFT MLG FIXED BRACE OTBD ATTACH POINT AFT FACE BUSHING HAS PITTING. INSTALLED BUSHINGS IAW DWG 5935812.
- [SDR DALA2016050903897](https://openairdocs.org/sdr/DALA2016050903897), May 5, 2016: BUSHING. DAMAGED. LEFT MLG, FORWARD FITTING, FORWARD LUG BUSHING HAS DAMAGE ON AFT FACE. REPLACED SPACER IAW DWG 5935812.
- [SDR DALA2016050903896](https://openairdocs.org/sdr/DALA2016050903896), May 5, 2016: ATTACH FITTING. CORRODED. LEFT MLG AFT ATTACH FITTING, FORWARD LUG, HAS PITTING ON AFT FACE OF BUSHING. REPLACED SPACER IAW DWG 5935812.
- [SDR DALA2016042003156](https://openairdocs.org/sdr/DALA2016042003156), Apr 19, 2016: LANYARD. UNSECURE. L1 DOOR SLIDE LANYARD HANGING. FOUND SLIDE HAD BEEN ACTIVATED AND DAMAGED. R & R SLIDE IAW WC 2561-4641.
- [SDR DALA2016102807903](https://openairdocs.org/sdr/DALA2016102807903), Sep 22, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520BT. REPLACED THE ACCESS PANEL.
- [SDR DALA2016102807902](https://openairdocs.org/sdr/DALA2016102807902), Sep 22, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520FT. REPLACED THE ACCESS PANEL.
- [SDR DALA2015092305826](https://openairdocs.org/sdr/DALA2015092305826), Sep 22, 2015: SKIN. DAMAGED. ELONGATED HOLES ON EXTERNAL FUSELAGE SKIN FROM BS 1098 TO 1136 BETWEEN LONGERONS 18 - 19R. REPAIRED IAW ERA 537809-14, REV O.
- [SDR DALA2015092105721](https://openairdocs.org/sdr/DALA2015092105721), Sep 20, 2015: WIRE. BROKEN. BROKEN WIRES ON LANYARDS OF R1 AND L2 DOOR SLIDES. R & R LANYARDS.
- [SDR DALA2015092005720](https://openairdocs.org/sdr/DALA2015092005720), Sep 19, 2015: DOOR FRAME. CRACKED. CRACK ON DOOR JAMB BELOW ANGLE AT NLG WHEEL WELL. CRACK WAS STOPPED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 AND 51-30-02.
- [SDR DALA2015091805706](https://openairdocs.org/sdr/DALA2015091805706), Sep 17, 2015: FRAME SPLICE. CORRODED. CORROSION ON FRAME SPLICE, BS 1503, LONGERON 22 - 24L. REPAIRED IAW ETI 90-15-075 AND ERA 537814-14, REV O.
- [SDR DALA2015091505705](https://openairdocs.org/sdr/DALA2015091505705), Sep 14, 2015: FRAME. WORN. WEAR ON FRAME, BS 1437. R & R WEB SECTION IAW DWG9912246.
- [SDR DALA2015091905718](https://openairdocs.org/sdr/DALA2015091905718), Sep 13, 2015: DOOR FRAME. CRACKED. CRACK ON NLG WHEEL WELL DOOR JAMB BEAM, BS Y=46 AND Y=17. REPAIRED IAW SRM 53-90-01.
- [SDR DALA2015091405645](https://openairdocs.org/sdr/DALA2015091405645), Sep 13, 2015: STRUCTURE. CORRODED. CORROSION ON HORIZONTAL STAB LT BARREL NUT HOLE NR 24. R & R IAW ERA 5377990-14, REV O.
- [SDR DALA2015091405644](https://openairdocs.org/sdr/DALA2015091405644), Sep 13, 2015: STRUCTURE. CORRODED. CORROSION ON HORIZONTAL STAB LT BARREL NUT HOLE, NR 10. REPAIRED IAW ERA 537790-14, REV O.
- [SDR DALA2016102807904](https://openairdocs.org/sdr/DALA2016102807904), Sep 12, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620MB. REPLACED THE ACCESS PANEL.
- [SDR DALA2015091305643](https://openairdocs.org/sdr/DALA2015091305643), Sep 12, 2015: SKIN. WORN. WEAR ON STRIP LT/RT FORWARD SIDE LOWER SKIN AT AFT ACCESSORY COMPARTMENT. DAMAGE REMOVED. FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-00-01, FIG 6 AND 51-30-20
- [SDR DALA2015091305642](https://openairdocs.org/sdr/DALA2015091305642), Sep 12, 2015: ANGLE. CRACKED. CRACK ON ANGLES AT BS 110, X=-7 AND -10, Z=-301, NOSE WHEEL WELL. REPLACED ANGLES IAW ERA 5912616, REV CK AND SRM 51-30-08.
- [SDR DALA2015091205641](https://openairdocs.org/sdr/DALA2015091205641), Sep 11, 2015: RUB STRIP. WORN. EXCESSIVE WEAR ON RUB STRIP SLAT PANEL NR 1 AND NR 2 INBD SIDE RT WING. REMOVED, FABRICATED AND INSTALLED NEW IAW SRM 51-30-02, 51-10-05.
- [SDR DALA2015091205640](https://openairdocs.org/sdr/DALA2015091205640), Sep 11, 2015: SKIN. DAMAGED. LIGHTNING STRIKE ON FUSELAGE SKIN BS 427-434 BETWEEN LONGERON 29-30R. EXCESSIVE DAMAGE. REPAIRED IAW SRM 53-30-02, 51-30-02, 51-10-03.
- [SDR DALA2015091105637](https://openairdocs.org/sdr/DALA2015091105637), Sep 10, 2015: SKIN. PUNCTURED. PUNCTURED SKIN ON FORWARD ACCESSORY COMPARTMENT DOOR LATERAL EDGE. REPAIRED IAW SRM 57-00-01.
- [SDR DALA2015091105636](https://openairdocs.org/sdr/DALA2015091105636), Sep 10, 2015: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL BETWEEN BS 1542-1554 LONGERON 24R. REMOVED AND REPAIRED THE INTERCOSTAL IAW SRM 51-10-01 AND DWG 9910087.
- [SDR DALA2016102807876](https://openairdocs.org/sdr/DALA2016102807876), Sep 9, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 520EB. REPLACED THE ACCESS PANEL.
- [SDR DALA2016102807875](https://openairdocs.org/sdr/DALA2016102807875), Sep 9, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 620EB. REPLACED THE ACCESS PANEL.
- [SDR DALA2015091105639](https://openairdocs.org/sdr/DALA2015091105639), Sep 9, 2015: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK BS 1281-1320. CUTOUT DAMAGE. PLUG WAS INSTALLED IAW SRM 53-40-01, 51-10-03.
- [SDR DALA2015091105638](https://openairdocs.org/sdr/DALA2015091105638), Sep 9, 2015: SUPPORT BRACKET. CORRODED. CORROSION ON RT EVACUATION SLIDE FITTING SUPPORT BRACKETS, 2 EA. EXCESSIVE DAMAGE. R & R FITTINGS IAW SRM 51-10-05, 51-10-03, 51-30-02 AND DWG 3936190.
- [SDR DALA2015091005635](https://openairdocs.org/sdr/DALA2015091005635), Sep 9, 2015: SKIN. DAMAGED. LIGHTNING STRIKE ON FUSELAGE SKIN, BS 178, BETWEEN STRINGERS 28 - 29L. REPAIRED IAW SRM 53-31-02, PARA 3C.
- [SDR DALA2015090905598](https://openairdocs.org/sdr/DALA2015090905598), Sep 8, 2015: RIB. CRACKED. CRACKED LEFT INBD L/E PANEL RIB OF HORIZONTAL STABILIZER. REPAIRED IAW SRM 55-00-01.
- [SDR DALA2015090905597](https://openairdocs.org/sdr/DALA2015090905597), Sep 8, 2015: SKIN. DENTED. DENT ON FUSELAGE SKIN, BS 223 BETWEEN LONGERONS 17 - 18L. REPAIRED IAW SRM 53-30-01, 51-30-02, 51-30-05 AND 51-10-03.
- [SDR DALA2015090905596](https://openairdocs.org/sdr/DALA2015090905596), Sep 8, 2015: CUSP WEB. DENTED. CORROSION ON LT CUSP WEB FROM BS 994 - 1003. REPAIRED IAW SRM 53-20-02.
- [SDR DALA2015090805594](https://openairdocs.org/sdr/DALA2015090805594), Sep 7, 2015: ANGLE. CRACKED. CRACK ON ANGLE AT WING BOX STRUCTURE AT BS 883, X=-41 AND Z=-9. REPAIRED IAW ERA 498192-14MA, REV A.
- [SDR DALA2015090805593](https://openairdocs.org/sdr/DALA2015090805593), Sep 7, 2015: SUPPORT FITTING. CORRODED. CORROSION ON LT FLAP SUPPORT FITTING HINGE INTERNAL STRUCTURE XW=154. REPAIRED IAW ERA 537789-14, REV O.
- [SDR DALA2015090805592](https://openairdocs.org/sdr/DALA2015090805592), Sep 6, 2015: WEB. CRACKED. CRACK ON WEB ABOVE FITTING BS XH 7.235 AT LT HORIZONTAL STAB INBD L/E. REPAIRED IAW SRM 51-00-02.
- [SDR DALA2015090705591](https://openairdocs.org/sdr/DALA2015090705591), Sep 6, 2015: CUSP WEB. CORRODED. CORROSION ON LT CUSP WEB MEMBRANE SURFACE, BS 757, X=60. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-02.

All 122: https://openairdocs.org/aircraft/N930DN/reports.md

## STCs that may be installed (OpenAirDocs) (119, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Mcdonnell Douglas MD-90-30)

- [STC ST02463AT](https://openairdocs.org/stc/ST02463AT): Installation of an Intrusion/Penetration Resistance Flightdeck Door and Reinforced Flightdeck Door Surround. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST03815AT-D](https://openairdocs.org/stc/ST03815AT-D): Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST03966AT](https://openairdocs.org/stc/ST03966AT): Lavatory refurbishment and PED power installation. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST04231AT](https://openairdocs.org/stc/ST04231AT): PED power installation. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC ST01541AT-D](https://openairdocs.org/stc/ST01541AT-D): Installation of Collins DLM-900 ACARS Management unit. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST04752NY](https://openairdocs.org/stc/ST04752NY): Replacement of Dual Analog Radio Altimeter Transceivers with Dual 5G Tolerant Collins Aerospace or Honeywell Digital Radio Altimeters Transceivers and Dual Shadin Digital-to-Analog Converters. S. LB Aircraft Engineering
- [STC ST09180AC](https://openairdocs.org/stc/ST09180AC): Installation of DeVore Wing Forward Position Lights. The Boeing Company
- [STC ST09181AC](https://openairdocs.org/stc/ST09181AC): Installation of main landing gear spotlights. The Boeing Company
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST00275LA](https://openairdocs.org/stc/ST00275LA): Installation of Passenger Service Cart. Safran Cabin Inc
- [STC ST01056LA](https://openairdocs.org/stc/ST01056LA): Installation of galleys, closet, stowage SIA, forward lavatory, bin, class divider (movable), sidewall and ceiling panels. Safran Cabin Inc
- [STC ST01336LA](https://openairdocs.org/stc/ST01336LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST01990LA-D](https://openairdocs.org/stc/ST01990LA-D): Installation of Overhead Stowage Bin Extension Kits. Safran Cabin Inc
- [STC ST01991LA-D](https://openairdocs.org/stc/ST01991LA-D): Interior Installations. Safran Cabin Inc
- [STC ST01998LA-D](https://openairdocs.org/stc/ST01998LA-D): Installation of Overhead Stowage Bin Kits. Safran Cabin Inc
- [STC ST02255LA](https://openairdocs.org/stc/ST02255LA): Modification and installation of Window Shades. Safran Cabin Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01818CH](https://openairdocs.org/stc/ST01818CH): Installation of a Honeywell Enhanced Ground Proximity Warning System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST02316CH](https://openairdocs.org/stc/ST02316CH): Upgrade of existing Mode S transponder installation to add enhanced surveillance Mode S. Amphenol Cable and Interconnect Technologies Inc
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST01932AT](https://openairdocs.org/stc/ST01932AT): Installation of SAF-T-GLO Aerospace Limited's photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST02928AT](https://openairdocs.org/stc/ST02928AT): Installation of a Honeywell Enhanced Ground Proximity Warning System (EGPWS). Woven Electronics LLC
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC SA9024NM-D](https://openairdocs.org/stc/SA9024NM-D): Installation of Scandinavian Bellyloading Company, sliding carpet loading system. SBC-America LLC
- [STC ST03276AT](https://openairdocs.org/stc/ST03276AT): Installation of a Honeywell MK II Aircraft Communications Addressing and Reporting System (ACARS). Woven Electronics, LLC
- [STC ST02896AT](https://openairdocs.org/stc/ST02896AT): Installation of a Kannad Model 406-AF Emergency Locator Transmittter (ELT). Woven Electronics LLC
- [STC ST01997CH](https://openairdocs.org/stc/ST01997CH): Installation of a Honeywell RESCU 406AF emergency locator transmitter (ELT) system. Honeywell International Inc
- [STC ST03988AT](https://openairdocs.org/stc/ST03988AT): Installation of the EMTEQ LED Lights in the main cabin. Woven Electronics LLC
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC ST03838AT](https://openairdocs.org/stc/ST03838AT): Installation of an Universal Avionics Application Server Unit (ASU) System Class II Electronic Flight Bag (EFB). Technical Aero Services Inc
- [STC ST03422NY](https://openairdocs.org/stc/ST03422NY): Update of Intelsat components. Delta Engineering Corporation
- [STC ST00491SE](https://openairdocs.org/stc/ST00491SE): Installation of the AlliedSignal Enhanced Ground Proximity Warning System. Honeywell International Inc
- [STC ST01023SE](https://openairdocs.org/stc/ST01023SE): Installation of a the TPA-81A Traffic Alert and Collision Avoidance System (TCAS) Processor in accordance with Master Drawing List 756-0119-001, Revision D, dated November 21, 2003, or later FAA approved revisions. Honeywell International Inc
- [STC ST01915AT](https://openairdocs.org/stc/ST01915AT): Installation of a RDR-4B Weather Radar/Windshear System. Honeywell International Inc
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04002AT](https://openairdocs.org/stc/ST04002AT): Installation of a Talon LED Replacement Wing and Tail Mounted Anti-Collision Lights. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST02541CH](https://openairdocs.org/stc/ST02541CH): Installation of an Aircell Broadband Services (ABS) System. Intelsat Inflight LLC
- [STC ST02532LA](https://openairdocs.org/stc/ST02532LA): Modify the wing fuel tanks access cover installation by replacing the existing rubstrip and seal with a new encapsulated wire mesh gasket and a new seal. Aviation Devices & Electronic Components LLC
- [STC ST02502LA](https://openairdocs.org/stc/ST02502LA): Installation of TDG Aerospace, Inc. Universal Fault Interrupter (UFI). TDG Aerospace Inc
- [STC ST04167CH](https://openairdocs.org/stc/ST04167CH): Installation of CMC CMA-5024 GLSSU units and ACSS NXT-800 Mode S Transponders. Canard Aerospace Corporation
- [STC ST04283AT](https://openairdocs.org/stc/ST04283AT): Interior Modification to add a Cart Stowage unit. Delta Air Lines Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC SA8339SW](https://openairdocs.org/stc/SA8339SW): Installation of a fuselage nose radome shell. The NORDAM Group LLC
- [STC ST01395AT-D](https://openairdocs.org/stc/ST01395AT-D): Installation of Collins DLM-700 B ACARS system installed with a Miltope Printer. HAECO Cabin Solutions LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC

All 119: https://openairdocs.org/aircraft/N930DN/stcs.md

## Related

- Other Mcdonnell Douglas MD-90-30 aircraft: https://openairdocs.org/model/mcdonnell-douglas-md-90-30/aircraft.md
- The IAE V2500SERIES engine: https://openairdocs.org/engine/iae-v2500series.md

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